Typhoon homer



Dec. 28, 1954 L. s. BlELlNSKl TYPHOON HOMER 2 Sheets-Sheet 1 Filed Jan. 30, 1951 INVENTOR. L60 5. fiz'ezz'zzs'kz,

ATTD RN EYE Dec. 28, 1954 1.. s. BIELINSKI 2,698,431

TYPHOON HOMER Filed Jan. 30, 1951 2 Sheets-Sheet 2 WWW -l I? INVENTOR.

L 90 5 356202 3 iii 54m wa,

ATTCI RN EYS United States Patent 6 TYPHOON HGMER.

Leos; Bielinski', Mingus, Tex. ApplicationJanuary-w; 1951 Serial No. 208,635-

' 1.Claim.. c1..34o. 34s

Th present invention relates :to a typhoon homer,. and. more; particularly .toa .device .to.. enable thepath of .a.

typhoonartmbe followed and .the; intensity thereof. indie CadQd-fit remote locations or stations.

One objectof; the. inventionisto provideadevice for enabling the path-ofa typhoorrtobe. followed ata remote. locatiomwhicln will. eliminatewthe. risk and. expense of reconnaissance-aircraft now generally used to obtain data. concerning; the. directional path .of. typhoons. and thelflse.

Another; object is, to provide a. device for obtaining meteorological. information .WhiCha can. he...conveniently and quickly dropped from an aircraft in..the. center .of .a

typhoonror: storm. soathat the. devicewill .transmit radiant ene giiirom the: eye of the stormandenable an accurate fixonthecenteror eye of the. storrn.at.all..times.

Another; object; is.-to-provide. a devicewhich will give reliable meteorological; data. on various. conditions; of.

eizgysignals when the; device strikesthe. water so thatthe.

signals..may be..-.receive.d at a remote. station and tram scribedwinto dataconeern-ing the intensity and. pathof the. storm or. typhoon.

Another obiectis. to. provide a typhoon homer which wiliiollow the path-of the storm from, thecenter or eye. andzwillitravel-along;in-the-center of thestorm so that thet-intermittentsig nals transmitted-will. always be from a location, at thecenter of the storm,zwhereby a fix onsaid.

signa-ls=-.at-., a .remote l'ocation will designate the eventual pathway-of.-.the storm.-v

Another:objeet isatoprovide a. device of the abovementioned type in-,.which theaintermittent signals. are timed to provide a definite beat, and the frequency of the signals is controlled-by the. barometric pressure conditions of the storm. Thus as the. barometric. pressure increases the frequency of the signals will increase correspondingly in amplitude;

Another object is to provide a meteorological device which can-be. dropped in the eye of a storm over water fmrnaanairplane which is provided with a captive balloon suclr that it;will have a tendency to seek the center of the whirlzof: the storm, and since the direction of the storm isscounter-clockwise a sail isprovided on the device which wiliiicontinuouslynrge the device toward the center or exact the storm. Thus, the device will be maintained in positiomclosezto or adjacent to the storm center in'such a manner that theradiantsignals emitted will be broadcast from the storm" center throughout its entire path.

Other. objects and advantages of the: invention Willbecomet-apparent during the course: offthetollowing' description of the accompanying drawings wherein:

Figure 1 is a side elevational view of the typhoon homer or meteorological device showing the manner in which the same is suspended from a parachute when the device is dropped from an aircraft in the center of a storm.

Figure 2 is a top elevational view illustrating the general shape of the device hull and showing the fixed sail for propelling: theadevice; toward the:- center ofthe :sto'mr throu-ghoutzthe stormapathwayir Eigure 3 is..alongitudinal crossvsectional*view takenozr linet 3-?n.of. Figuresilanddookingr in: the: direction of the arrows: to;illustrate various. structu-ral' details of the hull and showinglthe. arrangement.-ot..the-radiantenergy trans-- mittenandtimenzas wellias its electrical energyi source.

Figure 4 is a vertical cross-sectional view taken on linew 44. of Eigure-3 and looking in .thedirectiomofi the arrows. .to illustrateihe sectional-shapeofi-the hull. of- 'thedevice and .the manner in whiclrzthe deckcover-isrsealed irnplacen. and

Figure-5 is; a.;.d.iagrammatic.viewof the. variousacontrol devices. for initially; releasing the: parachute and .thereaf t'er transmitting. intermittent. radiant; energy signals,.=thefi equencyof. which is; controlled by? barometric pressureresponsive. mechanism;.

In. the. drawings wherein fOIf-thfi purposerofnconven ience ot' illustratiomzattention is directed-first totl igure.-l

whereinthe. typhoon homer: is generally. indicated: bythe reference, character 5; which when dropped from. an:- air craft is suspended from a parachute (not shown)- -havin g-;..shrouds;.6,. the lower. ends; of. which. are. connected to a terminal 1havingrsuspensinnrropesift... Whenithe device. is dropped. from. an. aircraft the. parachute (not shown.)-

opens; in.- the-.ausual; wayyand retards. the: descentof ihe.

typhoon homer or meteorological device 5. Thea'devicefi comprises ahul-Lstructure: including mflat bottom. 9 having sides.v mswhichaareconnected. atatherear:

by a stern-ll. and .atithe frontby a prnwa 1 2;. Theizhnlil structure 5 of thevdevicejshollow-and is providethwith;'v adeclc 13;. which .is;se.cured to thesidesg. stern.:anck proxy.

by machine. screws. 14: which-rare.- received inzcorrespond;

ingly threaded. internal. bcres;.15:.. A.sealing stripwfld ise interposed between.- the. hull 5 and .deck lirto. exclude. moisture: and prevent water from; entering the .hull. when.

the-device. is droppedina-bodyofi water 17 such=asan oeeanor the like, in;which aityphoomor othen'storrniisz present. It: is. intended .to drop I the. meteorologicab device or. typhoon. homer: overabody'oi': water suchuasrair ocean.

or. the like. from-arr aircraftfase the same approachesior enters thecenter. ofia typhoon .onsimilar storm. V

A captivezballoon. 2.0K is..-prov-iried for a.purpose:.which.

will..b.e hereinafter. morexfully. described; and. ismconanected toathe deck 13 ofthetyphoonhomer by arr-telecatrical cable.- 21 whichis: employed asamantennwfor-the: radiant energy transmitterand; in addition: holds: the

meteorological device- 5'-in thecenter of the storm-by.

reasomof the fact that'itis filled witha gas; li'gh'tenthan. air, andis moved toward the-center: oi thestormrby a centripetal force. The antenna; cable. 21 :iszsecured .to. the; deck 13.- bymeans: ot a clamping;hushing-lzrfand. extends. through; the. bushing :into; the; 11111115; Thedower; ends of the-suspensioncables: 81 0f the-shrouds 6.:arezscon-- nected to the machine screws. 14 and. interposed inzsaid.

suspensioncabl'es are disruptive.sleeves.:23 havingnameX-u plosive charge which-;.is. adapted to. beuignitedrfromt the.

electrical energy source when. the. initialradiant energy signal is. transmitted. TheeXplosion-charge. in the dis.

ruptive devices .23.:ca-uses the. cables 8 to .become detached.

from the hull 5-ineorder. tofreez-the parachuteafter the hull descends. into the waterqandkfioats: omthe-surface.

thereof;

A venttube 25: has its lower; end. mounted inthe: deck. 13 and its upper; end' providedzwith a vent-.cap 26. to. permit air. passage: to the interior'of thewhullaas indicated by the arrows in Figure 3. ventilator tubeZS is a collar 27, which. is secured in;tlre deck. 13, and said collar-isiprovidedwith.acentralgopem ing 28; for receiving. a mast--29; on which isz'mountedta. fixed sail 30 formed-of rigidumaterial-zv A set. SCICW'TSII. is mounted in theqcollar 27 to-hold themasti29'inr-place. and permit the same. to: be: adjusted. to predetermined angular positions. Normally,;'the sail Sit-isplaccd at an angle of approximately 30 degrees across a line of equal pressure (isobar) with relation to the storm center. Thus, since the storm whirl is counter-clockwise the resultant force of the storm whirl will propel the hull of the device in a direction toward the storm center constantly throughout its change in angular position.

The antenna cable 21 is adapted to be wound on a reel Patented. Dec... 2.8, 1954a Mounted rearward; of the-:-

'35 mounted on a reel bracket 36 secured to the deck 13 by bolts or machine screws 37. The reel 35 is provided with a hook '65 to which is adapted to be temporarily attached the antenna cable 21 at a point intermediate its ends so that the captive balloon 20 may be held close to the deck 13 when being transported to the desired stormarea in the aircraft. Suitable latching means may be provided for the reel 35 which can be released when the meteorological device is released from the aircraft so that the balloon 20 during the descent of the device will be projected by reason of the uncoiling of the antenna cable 21.

The radiant energy transmission device and control mechanism is generally indicated as at 40 and includes a casing 41 having a removable cover 43 (Fig. 3). The casing 41 is floatingly mounted within the hull to absorb shocks and is suspended from elastic cables 44 connected to the side walls of the hull at the top and bottom as at 45. The intermediate portions of the elastic cables 44 are attached to the casing 41 by suitable fastening elements 46. The antenna lead-in 48 is connected to the antenna cable 21 and enters the transmission and timer casing 41 as at 49. Also mounted in the hull 5 is a direct current source 50 which includes a casing 51 allliiixed to the bottom wall of the hull by screws or the A waterproof sheathed cable 53 extends between the battery casing 51 and the transmission and timer casing 41 to prevent short circuiting of the supply cable should the same become damp or moist from weather conditions. 7

Attention is directed to Figure 5 wherein there is shown diagrammatically the radiant energy transmitter and the various controls thereof and in circuit therewith. The radiant energy transmitter 40 includes a conventional radio-frequency oscillator to generate a frequency carrier wave, and the oscillator includes conventional inductance and capacitators which are inductively coupled to the antenna circuit and to the antenna 21 by the leadin cable 48. The source of electrical energy 50 may include a storage battery of approximately 12 volts which is connected to the vibrator and step-up transformer (not shown) in the transmitter casing 40 to supply the plate circuit with a stepped-up direct current source of approximately 300 volts. The vibrator being of conventional type and provided with multiple contacts is connected to the transformer to rectify the alternating current from the transformer. Such vibrator and step-up transformer units are of conventional design and are provided for mobile communication units for providing the plate circuit of a transmitter or the like with a stepped-up voltage from a low voltage direct current source. As shown in Figure 5, the battery 50 is connected to the vibrator by a cable 55 and the other terminal of the battery is connected by a cable 56 to a timer 57. The timer 57 is adapted to periodically make and break the circuit through the radio-frequency oscillator and includes a clock train mechanism for operating a cam controlled switch. The movable contact of the switch is connected to a cable 58 which is attached to the terminal 59 of an adjustable resistor blade 60 pivoted as at 61 and having one of its ends in contactual engagement with a resistor winding 62. One terminal of the resistance winding being connected to the inductance in the radio-frequency oscillator (not shown) by an electrical connection 63. Thus, the amplitude of the frequency of the radio-frequency transmitter will vary according to variations in the movement of the resistor blade, and when the resistance in the radio-frequency oscillator circuit is varied.

In order to operate the resistor blade 60 a barograph 65 of the sylphon type has its control shaft 66 in engagement with the outer end of the resistor blade 60. Thus, changes in atmospheric pressure existing in the center of the storm area will shift the resistor blade 60 and change the resistance in the radio frequency oscillator circuit and produce radiant energy signals at various amplitudes.

The timer 57 is provided with a cable 67 which is attached to the switch arm of the circuit maker and breaker,

QCVICGS 13 by means 01'. a C3016 06 IO lgnllfi a Small CX- ploslve charge 111 the disruptive device and thus tree the suspension cables 6 and me-parachute rrom the hull 5. the arrangement is such that on the first or initial circult closing position or the timer 57 the explosive charge in each or the disruptive devices 23 will be set 011' simultaneously.

'lhe nlament circuit (not shown) for the radio-frequency oscillator tubes is supplied trom the low voltage energy source in the conventional manner.

in operation, the hull 5 with the parachute (not shown) and balloon attached is dropped or released from an aircraft over a body of water close to the center of a typnoon or storm area. When the hull 5 lands in the body of water the captive balloon 20 is pro ected from its retracted position by reason of the fact that it unwinds from the drum 35 during descent. Upon the first or initial closing or the periodic switch governed by the timer 57, the explosive charges in the disruptive devices 23 are ignited to release the parachute. Simultaneously, the first radiant energy signal will be transmitted due to the closing or the circuit through the cables and 63 to the radio-frequency oscillator 40. This signal is received at one or more weather bureau stations to enable a fix to be obtained upon the pathway or the storm. The land stations may employ an oscillograph to determine the amplitude of the Irequency of the oscillations depending upon the barometric pressure in the storm area as previously described.

The balloon 20 and sail 30 maintain the hull 5 in the 4 storm center and thus, radiant energy signals transmitted periodically will enable the land station to obtain a fix on the device and thus obtain accurate data as to the longitude and latitude of the storm and its pathway direction. It will thus be seen that the hull of the typhoon homer will follow the storm center throughout its movement in any direction and will periodically transmit radiant energy signals during the storm movement so that an accurate fix can be obtained which will give the exact location and the direction of the storm pathway.

Iclaim: A device for indicating the path of a typhoon, comprising a hollow hull including a bottom, sides, a stern and a prow, a deck secured to said hull, an electrical cable:

having its lower end secured to said deck and providing an antenna, a captive balloon connected to the upper end of said cable, securing elements extending upwardly from said deck, parachute suspension cables connected to said securing elements, disruptive sleeves interposedin said suspension cables, a mast extending upwardly from said deck, a fixed sail secured to said mast, a radiant energy transmlssion device and control mechamsm comprising a casing floatingly mounted in said hull and having said antenna cable connected thereto, a current source positioned in said hull and electrically connected to said casing, a radio-frequency oscillator positioned insaid casing, a variable resistor connected to said oscillator, and a barograph for varying said resistor.

References Cited in the file of this patent UNITED STATES PATENTS Great Britain May 11,1907. 

